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Aircraft equipped with either a single or dual fuel quantity gauge installation must have the placard installed.
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The flight manual supplement titled "Supplement No. 2 to aircraft flight manual dated October 23, 1952" concerning the installation of the optional auxiliary fuel tank on affected model aircraft may contain erroneous information.
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Instructions to eliminate slackness in both the right and left rudder cables.
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Changing the stabilizer adjustment cable fiber rub block to a pulley arrangement to prevent cable slippage and possible cable fraying.
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Suggestions to alleviate troubles with the stabilizer adjusting mechanism.
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Inspecting the clearance between the engine mount and the tail pipe, and the entire nose wheel steering control system, between the nose wheel and the rudder pedals, also be checked for adequate clearances.
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Solution for cigarette lighter popping out of its socket after becoming fully heated.
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Points to remember when conducting routine inspections of the oil cooler lines and fittings.
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The decal originally attached to the propellers of aircraft indicated by the above serial numbers is incorrect. The incorrectly marked decal must be removed and replaced with the correctly marked decal.
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Modification and reinforcement of landing gear to prevent cracks in the leading edge of the streamlined tube where it joins the inboard end of the axle.